wing load distribution
wing load distribution
(OP)
Dear Readers,
If chordwise & spanwise CP distribution is known, nodal load can be evaluated on each node on the Fe model. If forces & moments are known at few locations (say 15 locations) on wing surface, what is proper way to distribute the load so that shear force, bending moment & torque diagram are same when done with Cp distribution.
thanks in advance
shearlag
If chordwise & spanwise CP distribution is known, nodal load can be evaluated on each node on the Fe model. If forces & moments are known at few locations (say 15 locations) on wing surface, what is proper way to distribute the load so that shear force, bending moment & torque diagram are same when done with Cp distribution.
thanks in advance
shearlag





RE: wing load distribution
i'd start with a standard wing spanwise load distribution, schrenk, which'll give you shear force and bending moment. tweek again to match your data.
RE: wing load distribution
shearlag
RE: wing load distribution
RE: wing load distribution